Defending Earth: the Threat from Asteroid and Comet Impact
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General Assembly Distr.: General 16 November 2012
United Nations A/AC.105/C.1/106 General Assembly Distr.: General 16 November 2012 Original: English Committee on the Peaceful Uses of Outer Space Scientific and Technical Subcommittee Fiftieth session Vienna, 11-22 February 2013 Item 12 of the provisional agenda* Near-Earth objects Information on research in the field of near-Earth objects carried out by Member States, international organizations and other entities Note by the Secretariat I. Introduction 1. In accordance with the multi-year workplan adopted by the Scientific and Technical Subcommittee of the Committee on the Peaceful Uses of Outer Space at its forty-fifth session, in 2008 (A/AC.105/911, annex III, para. 11), and extended by the Subcommittee at its forty-eighth session in 2011 (A/AC.105/987, annex III, para. 9), Member States, international organizations and other entities were invited to submit information on research in the field of near-Earth objects for the consideration of the Working Group on Near-Earth Objects, to be reconvened at the fiftieth session of the Subcommittee. 2. The present document contains information received from Germany and Japan, and the Committee on Space Research, the International Astronomical Union and the Secure World Foundation. __________________ * A/AC.105/C.1/L.328. V.12-57478 (E) 041212 051212 *1257478* A/AC.105/C.1/106 II. Replies received from Member States Germany [Original: English] [29 October 2012] The national activities listed below are based on the strong involvement of the Institute of Planetary Research of the German Aerospace Centre (DLR). DLR uses the Spitzer SpaceTelescope of the National Aeronautics and Space Administration (NASA) for an infrared survey (“ExploreNEOs”) of the physical properties of 750 near-Earth objects, as part of an international team. -
AAS/DPS Poster (PDF)
Spacewatch Observations of Asteroids and Comets with Emphasis on Discoveries by WISE AAS/DPS Poster 13.22 Thurs. 2010 Oct 7: 15:30-18:00 Robert S. McMillan1, T. H. Bressi1, J. A. Larsen2, C. K. Maleszewski1,J. L. Montani1, and J. V. Scotti1 URL: http://spacewatch.lpl.arizona.edu 1University of Arizona; 2U.S. Naval Academy Abstract • Targeted recoveries of objects discovered by WISE as well as those on impact risk pages, NEO Confirmation Page, PHAs, comets, etc. • ~1900 tracklets of NEOs from Spacewatch each year. • Recoveries of WISE discoveries preserve objects w/ long Psyn from loss. • Photometry to determine albedo @ wavelength of peak of incident solar flux. • Specialize in fainter objects to V=23. • Examination for cometary features of objects w/ comet-like orbits & objects that WISE IR imagery showed as comets. Why Targeted Followup is Needed • Discovery arcs too short to define orbits. • Objects can escape redetection by surveys: – Surveys busy covering other sky (revisits too infrequent). – Objects tend to get fainter after discovery. • Followup observations need to outnumber discoveries 10-100. • Sky density of detectable NEOs too sparse to rely on incidental redetections alone. Why Followup is Needed (cont’d) • 40% of PHAs observed on only 1 opposition. • 18% of PHAs’ arcs <30d; 7 PHAs obs. < 3d. • 20% of potential close approaches will be by objects observed on only 1 opposition. • 1/3rd of H≤22 VI’s on JPL risk page are lost and half of those were discovered within last 3 years. How “lost” can they get? • (719) Albert discovered visually in 1911. • “Big” Amor asteroid, diameter ~2 km. -
NASA's Near-Earth Object Program
NASA’s Near-Earth Object Program (Spaceguard) Don Yeomans Manager, NASA Near-Earth Object Program Office Meteor Crater Arizona History of Known NEO Population The Inner Solar System in 2006 201118001900195019901999 Known • 500,000 Earth minor planets Crossing •7750 NEOs Outside • 1200 PHAs Earth’s Orbit Scott Manley Armagh Observatory NASA’s NEO Search Program (Current Systems) Minor Planet Center (MPC) • IAU sanctioned NEO-WISE • Int’l observation database • Initial orbit determination www.cfa.harvard.edu/iau/mpc. html NEO Program Office @ JPL • Program coordination JPL • Precision orbit determination Sun-synch LEO • Automated SENTRY www.neo.jpl.nasa.gov Catalina Sky Pan-STARRS LINEAR Survey MIT/LL UofAZ Arizona & Australia Uof HI Soccoro, NM Haleakula, Maui3 The Importance of Near-Earth Objects •Science •Future Space Resources •Planetary Defense •Exploration NASA’s NEO Program Office at JPL Coordination and Metrics Automatic orbit updates as new data arrive SENTRY system Relational database for NEO orbits & characteristics Conduct research on: Discovery efficiency Improving observational data Modeling dynamics Optimal mitigation processes Impact warnings & outreach http://www.jpl.nasa.gov/asteroidwatch / NEO Program Office: http://neo.jpl.nasa.gov/ Near-Earth Asteroid Discoveries Start of NASA NEO Program Discovery Completion Within Size Intervals 40% 8% <1% 87% JPL’s SENTY NEO Risk Page http://neo.jpl.nasa.gov/risk/ Object Year Potential Impact Velocity H Estimated Palermo Torino Designation Range Impacts Prob. (km/s) (mag.) Diameter -
Modelización De Cráteres De Impacto
–– Modelización de cráteres de impacto Autores: Jesús Ordoño y Carlos Tadeo Tutor: Joan Alberich Institut Frederic Mompou Sant Vicenç dels Horts Modelización de cráteres de impacto Jesús Ordoño, Carlos Tadeo ÍNDICE Motivación y agradecimientos 2 Proceso de elaboración del Trabajo de Investigación y objetivos científicos alcanzados 4 1. Asteroides, meteoritos, cometas y cráteres de impacto 6 2. Modelización de cráteres de impacto 13 2.1. Introducción 13 2.2. Material utilizado 16 2.2.1. Datos de las canicas 17 2.2.2. Datos de la superficie de impacto 22 2.2.3. Dispositivo de lanzamiento 23 2.3. Procedimiento 25 2.4. Resultados obtenidos 28 2.4.1. Relación de los cráteres con el diámetro de las canicas 28 2.4.2. Relación de los cráteres con la masa y la densidad de las canicas 40 2.4.3. Relación de los cráteres con la energía cinética de las canicas 42 2.4.4. Relación de la profundidad de los cráteres con el diámetro de los mismos 45 3. Aplicación del modelo de cráteres de impacto a cráteres reales de la Tierra 47 3.1 Aplicación del modelo de cráteres de impacto en meteor Crater de Arizona: parámetro de control 48 3.2. Determinación del diámetro del meteorito en cráteres terrestres 51 3.3. Peligros espaciales: medidas de posibles cráteres producidos por asteroides cercanos a la Tierra 69 4. Aplicación del modelo de cráteres de impacto en otros cuerpos del Sistema Solar 81 4.1. Cráteres en planetas interiores 81 4.2. Cráteres en satélites de planetas exteriores 85 Conclusiones 89 Bibliografía 91 1 Modelización de cráteres de impacto Jesús Ordoño, Carlos Tadeo Motivación y agradecimientos Este estudio de los cráteres de impacto se gestó a raíz de nuestro interés por temas de astrofísica. -
Final Report
Final Report Project No: 282703 Project Acronym: NEOShield Project Full Name: A Global Approach to Near-Earth Object Impact Threat Mitigation Final Report Period covered: from 01/01/2012 to 31/05/2015 Date of preparation: 06/07/2015 Start date of project: 01/01/2012 Date of submission (SESAM): 05/08/2015 Project coordinator name: Project coordinator organisation name: Prof. Alan Harris DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV Version: 2 Final Report PROJECT FINAL REPORT Grant Agreement number: 282703 Project acronym: NEOShield Project title: A Global Approach to Near-Earth Object Impact Threat Mitigation Funding Scheme: FP7-CP-FP Project starting date: 01/01/2012 Project end date: 31/05/2015 Name of the scientific representative of the Prof. Alan Harris DEUTSCHES ZENTRUM project's coordinator and organisation: FUER LUFT - UND RAUMFAHRT EV Tel: +493067055324 Fax: +493067055303 E-mail: [email protected] Project website address: www.neoshield.net Project No.: 282703 Page - 2 of 44 Period number: 3rd Ref: 282703_NEOShield_Final_Report-13_20150805_154413_CET.pdf Final Report Please note that the contents of the Final Report can be found in the attachment. 4.1 Final publishable summary report Executive Summary NEOShield was conceived to address realistic options for preventing the collision of a naturally occurring celestial body (near-Earth object, NEO) with the Earth. Three deflection techniques, which appeared to be the most realistic and feasible at the time of the European Commission’s call in 2010, form the focus of NEOShield efforts: the kinetic impactor, in which a spacecraft transfers momentum to an asteroid by impacting it at a very high velocity; blast deflection, in which an explosive, such as a nuclear device, is detonated near, on, or just beneath the surface of the object; and the gravity tractor, in which a spacecraft hovering under power in close proximity to an asteroid uses the gravitational force between the asteroid and itself to tow the asteroid onto a safe trajectory relative to the Earth. -
Electrostatic Tractor for Near Earth Object
59th International Astronautical Congress, Paper IAC-08-A3.I.5 ELECTROSTATIC TRACTOR FOR NEAR EARTH OBJECT DEFLECTION Naomi Murdoch†, Dario Izzo†, Claudio Bombardelli†, Ian Carnelli†, Alain Hilgers and David Rodgers †ESA, Advanced Concepts Team, ESTEC, Keplerlaan 1, Postbus 299,2200 AG, Noordwijk ESA, ESTEC, Keplerlaan 1, Postbus 299,2200 AG, Noordwijk contact: [email protected] Abstract This paper contains a preliminary analysis on the possibility of changing the orbit of an asteroid by means of what is here defined as an “Electrostatic Tractor”. The Electrostatic Tractor is a spacecraft that controls a mutual electrostatic interaction with an asteroid and uses it to slowly accelerate the asteroid towards or away from the hovering spacecraft. This concept shares a number of features with the Gravity Tractor but the electrostatic interaction adds a further degree of freedom adding flexibility and controlla- bility. Particular attention is here paid to the correct evaluation of the magnitudes of the forces involved. The turning point method is used to model the response of the plasma environment. The issues related to the possibility of maintaining a suitable voltage level on the asteroid are discussed briefly. We conclude that the Electrostatic Tractor can be an attractive option to change the orbit of small asteroids in the 100m diameter range should voltage levels of 20kV be maintained continuously in both the asteroid and the spacecraft. INTRODUCTION would be transferred and the centre of mass of the system would be unaltered. In the original paper by The possibility of altering the orbital elements of an Lu and Love [6] a deflection of a 200m asteroid using asteroid has been discussed in recent years both in a 20 ton Gravitational Tractor is taken as a reference connection to Near Earth Object (NEO) hazard mit- scenario and a lead time of 20 years is derived to be igation techniques (asteroid deflection) [1] and to the necessary. -
Workshop on Communicating About Asteroid Impact Warnings and Mitigation Plans
Workshop on Communicating About Asteroid Impact Warnings and Mitigation Plans Workshop Report Prepared for the International Asteroid Warning Network September 2014 Executive summary In September 2014, Secure World Foundation hosted a two-day workshop on communication about near-Earth object (NEO) hazards and impact mitigation. The workshop was organized at the request and for the benefit of the International Asteroid Warning Network (IAWN), an international group of organizations involved in detecting, tracking, and characterizing NEOs. IAWN was organized in response to a United Nations (UN) recommendation and operates independently of the UN. The workshop brought together a diverse group of experts from the NEO science, risk communication, policy, and emergency management communities to provide communication guidance and advice to managers and directors of IAWN member programs and institutions. Prepared for IAWN, this workshop report captures key findings and recommendations derived from the workshop. Through brief presentations and case studies, guided discussion and breakout-group work, participants identified the following findings: The fundamental principles of risk communication are well defined and widely embraced. IAWN can draw on these principles in developing its communication strategy and plans. Cultivating and maintaining public trust, issuing notifications and warnings in a timely fashion, maintaining transparency in communications, understanding its various audiences, and planning for a range of scenarios are important to effectively communicate NEO impact hazards and risks. IAWN needs to operate as a global, round-the-clock communications network in order to become a trusted and credible source of information. Quantitative and probabilistic scales are of limited value when communicating with non- expert audiences. -
Investigating the Efficacy of Smallsats for Asteroid Detection
Investigating the Efficacy of CubeSats for Asteroid Detection Conor O’Toole 14204794 Goals • To investigate if CubeSats could be used to detect asteroids which could be classified as Near Earth Objects (NEOs), ie. that will come within 1.5AU of Earth at some point. • A number of factors must be taken into account: • Size limit on asteroids? • Max distance for detections? • One or multiple satellites? • Comparison with ground-based surveys Asteroids • Left-overs from Solar System formation • Primarily located in asteroid belts, but many occupy other orbits • Rate of collision with the planets and moons considered roughly constant • Ample evidence throughout Solar System Figure 1: Surfaces of Mercury, Moon, Mars, along with Barringer Crater in Arizona. [1], [2], [3], [4] NEOs • ~13,000 NEOs currently catalogued • 1km scale would cause destruction on a global scale. • Objects as small as 140m considered a major threat (in light of Chelyabinsk, Tunguska, etc) • Mitigation techniques in development (eg. Gravity tractor, kinetic impactor, etc) Figure 2: NEOs discovered against predicted • Primary concern remains detection values, for a range of sizes. [5] Asteroid Surveys • SpaceGuard (1998-2008) • Prioritised kilometre scale objects • CSS, LINEAR ~ 7,500 discoveries by 2014 ([6], [7]) • ATLAS (late 2015) • Early warning system for objects as small as 120m [8] • MANOS (2013-present) • Study physical parameters [9] • Space-based • NEOSSat, launched 2013 [10] • Sentinel, planned launch 2018 [11] LightForce Simulation • Space debris mitigation proposal [12-14] • Collision avoidance through ground-based laser stations • Simulation predicts roughly 90% reduction in number of collisions in the next year • Currently being extended to 100 years Figure 3: The general technique a LightForce station, either speeding up or slowing down an object to alter it’s orbit. -
Near-Earth Object Resource
NEO Resource Near-Earth Object Resource Compiled and edited by James M. Thomas for the Museum Astronomical Resource Society http://marsastro.org and the NASA/JPL Solar System Ambassador Program http://www.jpl.nasa.gov/ambassador Updated July 15, 2006 Based upon material available through the NASA Near-Earth Object Program http://neo.jpl.nasa.gov/ 1 of 104 NEO Resource Table of Contents Section Page Introduction & Overview 5 Target Earth 6 • The Cretaceous/Tertiary (K-T) Extinction 9 • Chicxulub Crater 10 • Barringer Meteorite Crater 13 What Are Near-Earth Objects (NEOs)? 14 What Is The Purpose Of The Near-Earth Object Program? 14 How Many Near-Earth Objects Have Been Discovered So Far? 15 What Is A PHA? 16 What Are Asteroids And Comets? 17 What Are The Differences Between An Asteroid, Comet, Meteoroid, Meteor and 19 Meteorite? Why Study Asteroids? 21 Why Study Comets? 24 What Are Atens, Apollos and Amors? 27 NEO Groups 28 Near-Earth Objects And Life On Earth 29 Near-Earth Objects As Future Resources 31 Near-Earth Object Discovery Teams 32 2 of 104 NEO Resource • Lincoln Near-Earth Asteroid Research (LINEAR) 35 • Near-Earth Asteroid Tracking (NEAT) 37 • Spacewatch 39 • Lowell Observatory Near-Earth Object Search (LONEOS) 41 • Catalina Sky Surveys 42 • Japanese Spaceguard Association (JSGA) 44 • Asiago DLR Asteroid Survey (ADAS) 45 Spacecraft Missions to Comets and Asteroids 46 • Overview 46 • Mission Summaries 49 • Near-Earth Asteroid Rendezvous (NEAR) 49 • DEEP IMPACT 49 • DEEP SPACE 1 50 • STARDUST 50 • Hayabusa (MUSES-C) 51 • ROSETTA -
Planetary Defense: an Overview
Planetary Defense: An Overview William Ailor, Ph.D. The Aerospace Corporation September 2011 © The Aerospace Corporation 2011 Background • Considerable work over the last several years on understanding the threat, proposing actions • 2004, 2007, 2009, 2011 Planetary Defense Conferences discussed – What we know about the threat to Earth from asteroids and comets – Consequences of impact – Techniques for deflection and disruption – Deflection mission design – Disaster mitigation – Political, policy, legal issues associated with mounting a deflection mission – Details and videos at www.planetarydefense.info, www.pdc2011.org • Highlights from 2011 IAA Planetary Defense Conference presented later in this briefing The Threat © The Aerospace Corporation 2011 Larger Meteor Events • 10 to 20 meteor impact events occur worldwide each day • 2 to 5 events/ day with potential for discovery by people • Injury has occurred, but rare October 9, 1992 March 27, 2003: Chicago (Park Forrest) • 27 March 2003, 05:50 UT (12:50 AM local time) Credit: Sgt. Kile - South Haven Indiana Police Department Prof. Peter Brown - University of Western Ontario • Southern suburbs of Chicago Dr. Dee Pack - The Aerospace Corporation • Camera in stationary squad car parked about 150 km away Video courtesy of University of Western Ontario, South Haven Indiana • Five structures damaged Police Department, and The Aerospace Corporation • Object estimated to be ~2 m in diameter, weigh ~7 tons Chicago (Park Forest) Impact, March 27, 2003 • Video image courtesy of ABC News, Channel 7, Chicago, IL. 6 Events June 30, 1908: Tunguska, Siberia • Airburst of ~30 m diameter object at ~6 km altitude 1.2 kilometer BARRINGER (OR METEOR) CRATER, Arizona, • 2-15 MT explosion was created about 49,000 years ago by a small nickel-iron asteroid (Photo by D.J. -
Impact Hazard Communication Risk Study: 2007 VK184 Laura Delgado
Impact Hazard Communication Risk Study: 2007 VK184 Laura Delgado López, Secure World Foundation Overview The 130-meter sized 2007 VK 184 was discovered in early November 2007 by the NASA-funded Catalina Sky Survey (CSS) at the University of Arizona. According to NASA, 2007 VK 184 was known to pose “the most significant risk of Earth impact over the next 100 years” with a rating of 1 in the Torino Scale, and a 1-in-1800 chance of impact in June 2048 with up to four potential impacts. Analysis was based on 101 observations that took place between 12 Nov 2007 and 11 Jan 2008,1 when the asteroid moved beyond view. It was sighted nearly six years later in March 2014 by Dr. David Tholen of the University of Hawaii who provided the new tracking data to the Minor Planet Center. NASA JPL’s “Sentry” system retrieved the observations and issued a when a new impact hazard assessment which concluded that no closer encounters are predicted for the foreseeable future. Given these observations, the NEO Program Office removed it from the Impact Risk Page. Coverage Media coverage of 2007 VK 184 focused on the initial discovery of the object in late 2007/ early 2008 and then on its demotion from a viable threat earlier this year. The object was mentioned in the intervening years in articles covering other objects, as one of few that represented non- negligible threats. Discovery On 30 December 2007 an Australian newspaper, The Age, reported the discovery in “Space rock on way, but don't panic yet” by Daniel Dasey. -
NEA Discovery, Orbit Calculation and Impact Probability Assessment
NEA discovery, orbit calculation and impact probability assessment Asteroid Grand Challenge Seminar Series Paul Chodas NASA NEO Program Office JPL/Caltech March 14, 2014 Asteroid 2012 DA14, Feb. 15, 2013 Chelyabinsk, Russia, Feb. 15, 2013 ~20-meter asteroid, 500 kt of energy released at ~30 km altitude http://neo.jpl.nasa.gov Current locations of large asteroids About 43,000 asteroids larger than Trailing 5 km (3 miles) Trojans are currently known. These are their positions as of today. Leading Only 20 of Main Belt Trojans these are NEAs, and only 2 are PHAs. Current Positions of all NEAs with Diam. > 1 km Current Positions of all NEAs with Diam. > 1 km + 300 of their orbits NASA’s NEO Search Programs Catalina Sky Pan-STARRS LINEAR Survey U of AZ U of HI MIT/LL Arizona & Australia Haleakala, Maui Soccoro, NM • Currently, most Near-Earth Asteroid discoveries are made by: Catalina Sky Survey (60%) and Pan-STARRS-1 (35%). • LINEAR is now retired, but was very productive at finding large NEAs. Discovery of 2012 DA14 • Discovered by an amateur Discovery Images, Feb. 22, 2012 astronomer in La Sagra, Spain using a state-of-the-art fast readout camera and detection software that looked for trails produced by fast-moving asteroids. • The asteroid was found in a less searched region of the sky. • Moderately faint: magnitude 18.8, and moving quite fast: 11 arc-sec per minute. Courtesy Jaime Nomen, La Sagra Observatory Sky Coverage, Feb.-Mar. 2014 Courtesy of Tim Spahr, Minor Planet Center Trajectory of Chelyabinsk Impactor Kepler’s Laws 1.